Overall aerodynamic and aerothermal design considerations for the Hermes space vehicle are summarized and a general methodology for the development of Hermes is outlined. Examples of specific design objectives are given which address the problems of longitudinal stability and vehicle aerodynamic heating.
Concepts Generaux Aerodynamiques-Aerothermiques d'Hermes (General Aerodynamic-Aerothermodynamic Concepts for Hermes)
1987
7 pages
Report
Keine Angabe
Englisch
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